Method for depositing highly erosive and abrasive wear resistant composite coating system on a substrate

Abstract

The method for producing the disclosed material comprises chemical vapor depositing on the substrate a substantially columnar, intermediate layer of tungsten and chemical vapor depositing on the intermediate layer a non-columnar, substantially lamellar outer layer of a mixture of tungsten and tungsten carbide. The tungsten carbide comprises W.sub.2 C, W.sub.3 C, or a mixture of both wherein the ratio of the thickness of the tungsten intermediate layer to the thickness of the outer layer is at least: (a) 0.35 in the case of tungsten plus W.sub.2 C in the outer layer, (b) 0.6 in the case of a mixture of tungsten and W.sub.3 C in the outer layer and (c) 0.35 in the case of mixtures of tungsten and W.sub.2 C and W.sub.3 C in the outer layer. The chemical vapor deposition steps are carried out at pressures within the range of 1 Torr to 1,000 Torr and temperatures within the range of about 300.degree. to about 650.degree. C.

Parent Case Text

This is a division of application Ser. No. 07/153,738, filed Feb. 8, 1988, now U.S. Pat. No. 4,855,188.

Description

BACKGROUND OF THE INVENTION

A. Field of the Invention

The invention relates to highly erosive and abrasive wear resistant composite coating. More particularly, the invention relates to an improved highly erosive and abrasive wear resistant coating comprising a composite coating system of an intermediate layer of substantially pure tungsten and an outer two phase layer of a mixture of tungsten and tungsten carbide.

B. Background Art

High hardness materials are widely used as coatings on various type of mechanical components and cutting tools. Such coatings impart erosion and abrasion wear resistance and thus increase the erosive and abrasive wear life of objects that have been coated. The high hardness materials can also be used to produce free standing objects which are erosive and abrasive wear resistant.

Chemical vapor deposition processes can be used to produce highly erosive and abrasive wear resistant hard coatings and free standing objects. In a typical chemical vapor deposition (CVD) process, the substrate to be coated is heated in a suitable chamber and then a gaseous reactant mixture is introduced into the chamber. The gaseous reactant mixture reacts at the surface of the substrate to form a coherent and adherent layer of the desired coating. By varying the gaseous reactant mixture and the CVD process parameters, various types of deposited coatings can be produced.

In U.S. patent application Ser. No. 092,809, filed 3 Sept. 1987, now U.S. Pat. No. 4,874,642, issued 17 Oct. 1989, extremely hard, fine grained, non-columnar, substantially lamellar tungsten/carbon alloys are described which are produced by chemical vapor deposition. The described alloys consist primarily of a mixture of a substantially pure tungsten phase and at least one carbide phase wherein the carbide phase consists of W.sub.2 C or W.sub.3 C or a mixture of W.sub.2 C and W.sub.3 C. The disclosed tungsten/carbon alloys are free of columnar grains and consist essentially of extremely fine, equiaxial crystals.

It has been found that the tungsten/carbon alloys such as those described in the aforementioned U.S. patent application, when deposited upon certain types of substrates, exhibit a very fine micro-crack system throughout the deposit. On many types of substrates and under many types of erosive and abrasive wear conditions, preferential attack occurs at the cracks, resulting in poor erosion and abrasion wear resistance for such coatings.

The use of an intermediate layer of substantially pure tungsten followed by a tungsten carbide coating is described in the prior art. For example, U.S. Pat. No. 3,389,977 discloses a method of depositing substantially pure tungsten carbide in the form W.sub.2 C wherein the adherence of W.sub.2 C to a steel substrate is improved by first cleaning the surface and then depositing a thin film of tungsten. The thin film of tungsten is deposited at or above 600.degree. C., making the use of the deposition process unsuitable for providing erosive and abrasive wear resistance coating on various carbon steels, stainless steels, nickel and titanium alloys without severely degrading their mechanical properties. Additionally, pure W.sub.2 C deposited according to this patent consists of columnar grains as opposed to non-columnar grains described in the present patent application. Other instances of the use of very thin tungsten intermediate layers, often as a diffusion layer, are reported in other prior art in order to improve adhesion of tungsten carbide on a substrate. However, there is no report in the prior art of the effect of a tungsten interlayer on coating properties of the final coating system nor has the effect of such a tungsten intermediate layer on the reduction or elimination of cracks in the outer coating been reported.

SUMMARY OF THE INVENTION

Very generally, the highly erosive and abrasive wear resistant composite coating system of the invention comprises an intermediate layer of tungsten and an outer layer of tungsten/carbon alloy coating. The intermediate layer of tungsten is of sufficient thickness to confer substantial erosive and abrasive wear resistance characteristics to the composite coating system. The outer tungsten/carbon alloy layer is comprised of a mixture of tungsten and tungsten carbide, with the tungsten carbide phase comprising of W.sub.2 C, W.sub.3 C or a mixture of both. The ratio of the thickness of the intermediate or inner layer to the thickness of the outer layer is at least above 0.3 in the cases of W+W.sub.3 C, W+W.sub.2 C+W.sub.3 C and W+W.sub.2 C coatings. Preferably the ratio of the thickness of the inner layer to the thickness of the outer layer to get optimum erosion and abrasion wear performance is at least 0.35 in the case of mixtures of tungsten and W.sub.2 C in the outer layer, 0.60 in the case of mixtures of tungsten and W.sub.3 C in the outer layer and, 0.35 in the case of mixtures of tungsten and W.sub.2 C and W.sub.3 C in the outer layer.

The tungsten/carbon alloys or coatings consisting of a mixture of tungsten and tungsten carbide, with the tungsten carbide phase comprising W.sub.2 C, W.sub.3 C or mixtures of both are defined herein as tungsten/tungsten carbide to simplify the description.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1 is the photomicrograph at 1,000 magnification of the tungsten coating on AM-350 stainless steel showing a rough surface finish but the absence of cracks.

FIG. 2 is the cross-sectional view at 3,000 magnification of the tungsten coating on AM-350 stainless steel showing columnar growth structure.

FIG. 3 is the schematic of the unetched cross-sectional view at 2,000 magnification of the composite coating system on AM-350 stainless steel substrate constructed in accordance with the invention.

FIG. 4 is the schematic of the cross-sectional view at 2,000 magnification of the composite coating system on AM-350 stainless steel etched with the murakami solution constructed in accordance with the invention.

FIG. 5 is the photomicrograph of the W+W.sub.3 C coating without the tungsten interlayer at 1,000 magnification on AM-350 stainless steel showing a network of interconnected cracks.

FIG. 6 is the photomicrograph of the W+W.sub.3 C coating with the tungsten interlayer at 1,000 magnification on AM-350 stainless steel showing a few interconnected cracks.

FIG. 7 is the photomicrograph of the W+W.sub.3 C coating with the tungsten interlayer at 1,000 magnification on AM-350 stainless steel showing the absence of cracks.

FIG. 8 is the photomicrograph of the surface of W+W.sub.3 C coating without the tungsten interlayer on AM-350 stainless steel at 100 magnification, scratched with a diamond stylus and showing significant loss of the coating in the 30-40 Newton load range.

FIG. 9 is the photomicrograph of the surface of W+W.sub.3 C coating with the tungsten interlayer on AM-350 stainless steel at 100 magnification, scratched with a diamond stylus and showing significantly reduced loss of the coating in the 30-40 Newton load range.

FIG. 10 is the photomicrograph of the W+W.sub.2 C+W.sub.3 C coating without the tungsten interlayer on AM-350 stainless steel at 1,000 magnification showing a network of cracks.

FIG. 11 is the photomicrograph of the W+W.sub.2 C+W.sub.3 C coating with the tungsten interlayer on AM-350 stainless steel at 1,000 magnification showing the absence of cracks.

FIG. 12 is the photomicrograph of the W+W.sub.2 C coating with the tungsten interlayer on AM-350 stainless steel at 1,000 magnification showing the presence of a fine crack.

FIG. 13 is the photomicrograph of the W+W.sub.2 C coating with the tungsten interlayer on AM-350 stainless steel at 1,000 magnification showing the absence of cracks.

FIG. 14 is the graph illustrating the relationship between the erosion rate and the ratio of the tungsten to the tungsten/carbon alloy coating thicknesses on AM-350 stainless steel, and

FIG. 15 is the graph illustrating the relationship between the tungsten/carbon alloy coating thickness and the ratio of the thicknesses of the tungsten layer to the tungsten/carbon alloy layer on AM-350 stainless steel.

DETAILED DESCRIPTION OF THE INVENTION

In a preferred form of the invention, the intermediate layer of tungsten is produced by chemical vapor deposition under sub-atmospheric to slightly atmospheric pressure, i.e., within the range of about 1 Torr. to about 1,000 Torr., at a temperature of about 300.degree. to about 650.degree. C., using a mixture of tungsten halide such as WF.sub.6, hydrogen, and an inert gas such as argon. The intermediate layer is of a sufficient thickness to confer substantial erosive and abrasive wear resistance characteristics on the composite system. The specific thickness necessary to do this for various composite coating systems will become readily apparent to those skilled in the art from the teaching of this specification, particularly in connection with the examples set forth below. The intermediate layer of tungsten should be at least about two microns thick and, for most systems, will be greater than about three microns.

Following deposition of the intermediate layer of substantially pure tungsten, an outer layer of tungsten/tungsten carbide is deposited under sub-atmospheric to slightly atmospheric pressure, i.e., within the range of about 1 Torr. to about 1,000 Torr., at temperatures in the range of about 300.degree. to about 650.degree. C. This outer layer may be either a two phase layer comprising tungsten and W.sub.2 C or tungsten and W.sub.3 C. Alternatively, this outer layer may be a three phase layer comprising tungsten, W.sub.2 C and W.sub.3 C. The relative proportions of the tungsten, W.sub.2 C, and W.sub.3 C may be selected in accordance with the particular properties desired in the final composite coating system. In order to achieve such proportions, the tungsten/tungsten carbide deposit is applied utilizing a flow of tungsten halide such as WF.sub.6, argon, hydrogen and an oxygen containing hydrocarbon such as dimethylether (DME). By controlling the temperature, W/C atomic ratio in the feed gas and the ratio of hydrogen to WF.sub.6 during the deposition reaction, the particular desired chemical composition of the tungsten/tungsten carbide layer may be obtained. Details of the foregoing described process may be found in applicant's U.S. patent application Ser. No. 92,809 now U.S. Pat. No. 4,874,642, issued 17 Oct. 1989.

In accordance with the present invention, it has been found that the ratio of the thickness of the inner tungsten layer to the thickness of the outer multi-phase tungsten/tungsten carbide layer has a profound affect on the erosive and abrasive wear resistance properties of the resulting composite coating system. Although the reasons for this improvement in the erosive and abrasive wear resistance are yet not fully understood, it is believed that the use of the tungsten intermediate layer together with the specified ratios set forth below refine the micro-crack structure in the outer deposit so that, even though preferential attack along the crack system occurs, the rate of attack is greatly attenuated. Moreover, as set out below, under certain conditions a crack free outer layer may be achieved.

More specifically, the ratio of the thickness of the inner tungsten layer to the thickness of the outer tungsten/tungsten carbide layer, in accordance with the composite coating system of the invention, is at least above 0.30 with the W+W.sub.3 C, W+W.sub.2 C+W.sub.3 C and W+W.sub.2 C coatings. More specifically, to obtain optimum erosion and abrasion wear performance the thickness ratio is at least: 0.35 in the case of mixtures of tungsten and W.sub.2 C in the outer layer, 0.60 in the case of mixtures of tungsten and W.sub.3 C in the outer layer, and 0.35 in the case of mixtures of tungsten and W.sub.2 C and W.sub.3 C in the outer layer. Using these minimum ratios, superior erosive and abrasive wear resistance can be achieved. Moreover, by using the ratios set forth above, under certain conditions, completely crack free outer layers may be achieved.

The inner tungsten layer is substantially columnar in its grain structure with the longer dimension of the grains extending generally perpendicular to the substrate surface. On the other hand, the grain structure of the tungsten/tungsten carbide outer layer is very fine-grained, equiaxed, non-columnar, and substantially lamellar typically of the order of one micron or less in size. Such structures may be readily achieved using the method described in the aforementioned U.S. patent application.

The present composite coating system of the invention can be deposited on a number of ferrous metals and alloys such as cast irons, carbon steels, stainless steels and high speed steels, non-ferrous metals and alloys such as copper, nickel, platinum, rhodium, titanium, aluminum, silver, gold, niobium, molybdenum, cobalt, tungsten, rhenium, copper alloys and nickel alloys such as inconel and monel, titanium alloys such as Ti/Al/V, Ti/Al/Sn, Ti/Al/Mo/V, Ti/Al/Sn/Zr/Mo, Ti/Al/V/Cr, Ti/Mo/V/Fe/Al, Ti/Al/V/Cr/Mo/Z and Ti/Al/V/Sn alloys, non-metals such as graphite, carbides such as cemented carbide, and ceramics such as silicon carbide, silicon nitride, alumina, etc. In depositing the composite coating system on reactive substrate materials, such as cast irons, carbon steels, stainless steels, high speed steels, and nickel and monel alloys, it is preferred to coat the substrate first with a more noble material such as nickel, cobalt, copper, silver, gold, platinum, palladium or iridium, by electrochemical or electroless techniques or by a physical vapor deposition technique such as sputtering. In depositing the composite coating system on reactive titanium or titanium alloys, it is also preferred to coat the substrate first with a more noble material described above by electroless technique or by physical vapor deposition technique such as sputtering. It is also preferred to coat the substrate first with a thin layer of a more noble material described above by electroless technique followed by another thin layer of a more noble material by electrochemical or physical vapor deposition technique. It is also preferred to clean the surface of the titanium or titanium alloy substrate first and heat treat the noble metal deposit after depositing on the substrate. The deposition of noble metal and subsequent heat treatment steps on titanium or titanium alloys are described in detail in U.S. patent application Ser. No. 139,891, filed 31 Dec. 1987 now U.S. Pat. No. 4,902,535, issued 20 Feb. 1990. It is also preferred that upper limit of the deposition temperature be about 525.degree. C. when depositing the present composite coating system on titanium and titanium alloys to minimize the degradation of the mechanical properties. No deposition of the noble material, however, is required for coating non-reactive materials such as copper, nickel, cobalt, silver, gold, platinum, rhodium, niobium, molybdenum, tungsten, rhenium, graphite, carbides and ceramics. Free standing parts of the composite coating of the present invention can be made by depositing it on the substrates such as copper, nickel, cobalt, silver, gold, molybdenum, rhenium, and graphite and then removing these substrates by grinding and chemical or electrochemical etching.

To further illustrate the present invention, the following data are set forth with respect to a number of coating systems.

A number of ferrous and non-ferrous metals and alloys were used as substrates in the following coating experiments. Specimens of AM-350 and SS-422 stainless steels Inconel and IN-718, a well known nickel alloy, were electroplated with 2 to 5 .mu.m thick nickel before coating them with tungsten and tungsten/tungsten carbide to protect them from the attack of hot and corrosive HF acid gas produced as a by-product in the CVD process. Specimens made of titanium alloy such as Ti/6Al/4V, on the other hand, were plated with 2 to 5 .mu.m thick nickel using an electroless technique described in detail in U.S. patent application Ser. No. 139,891, filed 31 Dec. 1987 now U.S. Pat. No. 4,902,535, issued 20 Feb. 1990 before coating them with tungsten and tungsten/tungsten carbide.

EROSION TEST PROCEDURE

The erosion resistance performance of the uncoated and the coated specimens was determined using a miniature sandblast unit; the test parameters are summarized in Table 1. The fine alumina powder, which was used as the erosive material, provided a very harsh erosion environment, as compared to sand erosion; consequently, an accelerated test procedure could be used. Two essentially equivalent techniques were used to evaluate the erosion resistance of the specimens. The first technique involved measuring the time it took for the erosive material to penetrate the tungsten/tungsten carbide coating, which is called the breakthrough time. Penetration of the tungsten/tungsten carbide coating was visibly apparent as a color change at the center of the erosion pit; the fact that this color change corresponded to the initial penetration of the tungsten/tungsten carbide coating was confirmed by microscopic examination of erosion pits in cross section. The second technique involved measuring the weight of a specimen that was lost during an erosion test for a given time; this time was always less than the breakthrough time so that only the weight loss of the coating was measured. The erosion rate was then calculated as the time required to penetrate the coating on a per mil basis or as the average weight loss for a 30 second erosion test, respectively.

EXAMPLES

EXAMPLE 1

Uncoated specimens of AM-350 stainless steel and Ti/6Al/4V were eroded with alumina for two minutes (120 seconds). The depth of the crater was measured to calculate the erosion rate. The calculated erosion rate was 60 and 50 seconds/mil for AM-350 and Ti/6Al/4V specimens, respectively.

EXAMPLE FOR TUNGSTEN COATING

EXAMPLE 2

A number of AM-350, Ti/6Al/4V and IN-718 specimens (0.095 inch.times.1 inch.times.2 inch) were placed in an inductively heated graphite furnace inside a gas-tight quartz envelope. The specimens were heated to 460.degree. C. in the presence of flowing argon gas and at the temperature a gaseous mixture of 300 cc/min of WF.sub.6, 3,000 cc/min of hydrogen, and 4,000 cc/min of argon was passed into the furnace over the specimens. The total pressure within the system was maintained at 40 Torr. The deposition was conducted for 15 minutes; thereafter, the flow of the reactive gases was stopped and the specimens were cooled.

The specimens were found to be coated with a dull, adherent, coherent, and uniform coating. The coating thickness on stainless steel specimens was .about.12 .mu.m on each side (see Table 2). The coating had a rough surface finish and was free of cracks, as shown in the FIG. 1. The coating consisted of columnar growth structure, as shown in the FIG. 2. X-ray diffraction analysis showed the presence of only tungsten in the coating. It had a hardness of 455 Vickers, as shown in Table 3. The coating showed very poor erosion performance; time required to penetrate the coating was only 3 seconds, resulting in a erosion rate of 6 seconds/mil. This, therefore, indicated that CVD tungsten could not be used to provide erosion protection.

TABLE 1 ______________________________________ Erosion Test Procedure ______________________________________ Nozzle Diameter 0.018 inch Stand off Distance 0.6 inch Erosion Media Fine Alumina Powder (50 .mu.m Average Particle Size) Supply Pressure 32 psig Flow Rate of Erosion 1.6 g/min Media Erosion Test Standard Breakthrough Time and Weight Loss ______________________________________

TABLE 2 __________________________________________________________________________ Example 2 Example 3 Example 4A Example 4B Example __________________________________________________________________________ 4C Experiment No. 50 36 37 33 42 Substrate AM-350 AM-350 AM-350 Ti/6A1/4V AM-350 AM-350 Ti-6A1/4V Temperature, .degree.C. 460 460 460 465 460 Pressure, Torr 40 40 40 40 40 W Coating Conditions H.sub.2, SCCM 3,000 -- 3,000 3,000 3,000 Ar, SCCM 4,000 -- -- -- -- WF.sub.6, SCCM 300 -- 300 300 150 Time, Min. 15 -- 5 5 30 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM -- 3,000 3,000 3,000 3,000 Ar, SCCM -- -- -- -- -- WF.sub.6, SCCM -- 300 300 300 300 DME, SCCM -- 40 40 40 40 Time, Min. -- 40 55 35 20 Coating Thickness, .mu.m Tungsten 12.0 -- 3.0 2.0 3.0 5.0 3.0 Tungsten/Tungsten Carbide -- 22.0 27.0 28.0 25.0 13.0 14.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide -- 0.0 0.11 0.07 0.12 0.38 0.21 Thickness Surface Topography Rough, Smooth, Smooth, Many Fine Smooth, Smooth, Many Fine No Cracks Many Fine Interconnected Many Fine Interconnected Interconnected Cracks Interconnected Cracks Cracks Cracks __________________________________________________________________________ Example 4D Example 4E Example 4F Example 4G Example __________________________________________________________________________ 4H Experiment No. 38 107 104 106 164 Substrate AM-350 AM-350 AM-350 Ti/6A1/4V AM-350 AM-350 Ti/6A1/4V IN-718 Temperature, .degree.C. 460 460 460 460 460 Pressure, Torr 40 40 40 40 40 W Coating Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 3,000 Ar, SCCM -- 4,500 4,500 4,500 4,500 WF.sub.6, SCCM 300 300 300 300 300 Time, Min. 10 15 15 15 25 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 3,000 Ar, SCCM -- 300 300 300 300 WF.sub.6, SCCM 300 300 300 300 300 DME, SCCM 40 30 50 40 40 Time, Min. 30 30 30 30 25 Coating Thickness, .mu.m Tungsten 8.0 8.5 9.0 8.0 9.0 16.9 17.1 16.9 Tungsten/Tungsten Carbide 16.0 12.5 11.5 11.0 11.0 14.5 13.3 11.7 Tungsten Coating Thickness Tungsten/Tungsten Carbide 0.50 0.68 0.78 0.73 0.81 1.17 1.29 1.44 Thickness Surface Topography Smooth, Smooth, A Few Smooth, A Few Fine Smooth, A Smooth, A Few Fine Several Fine Fine Inter- Interconnected Few Fine Interconnected Inter- Connected Cracks Interconnected Cracks connected Cracks Cracks Cracks __________________________________________________________________________ Example 4I Example 4J Example 4K __________________________________________________________________________ Experiment No. 177 167 160 Substrate AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V IN-718 Temperature, .degree.C. 460 460 460 Pressure, Torr 40 40 40 W Coating Conditions H.sub.2, SCCM 2,500 3,000 2,500 Ar, SCCM 6,000 4,500 6,000 WF.sub.6, SCCM 250 300 250 Time, Min. 25 25 25 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 Ar, SCCM 2,000 300 2,000 WF.sub.6, SCCM 300 300 300 DME, SCCM 40 40 40 Time, Min. 35 20 15 Coating Thickness, .mu.m Tungsten 11.0 10.5 10.3 15.5 15.7 15.0 13.2 12.5 12.5 Tungsten/Tungsten Carbide 7.7 7.8 7.7 8.7 9.0 9.0 4.4 3.4 4.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide 1.42 1.35 1.34 1.78 1.74 1.67 3.00 3.67 3.12 Thickness Surface Topography Smooth, A Few Fine Smooth, A Few Fine Smooth, No Cracks Interconnected Interconnected Cracks Cracks __________________________________________________________________________

EXAMPLE FOR TUNGSTEN/TUNGSTEN CARBIDE (W+W.sub.3 C) COATING

EXAMPLE 3

In this example, several specimens of AM-350, Ti/6Al/4V and IN-718 were coated simultaneously in a single run. The specimens were heated to a temperature of about 460.degree. C. in the presence of flowing argon and at the reaction temperature a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min of hydrogen and 40 cc/min of DME was passed into the furnace over the specimens. The total pressure was maintained at 40 Torr, as shown in Table 2. The deposition was conducted for 40 minutes.

All the specimens were coated with a bright, smooth, adherent, coherent and uniform coating. The coating thickness on stainless steel specimens was .about.22 .mu.m. The coating consisted of a mixture of W and W.sub.3 C phases, as determined by x-ray diffraction. It was free of columnar grains. The coating had a smooth surface finish. However, the surface of the coating was heavily cracked, as shown in the FIG. 5. The coating had a hardness of 1788 Vickers, as shown in Table 3. The coating showed poor erosion resistance; the breakthrough time and erosion rate were 36 seconds and 42 seconds/mil, respectively. The weight loss during erosion test was 0.00036 g in 30 seconds. Extensive chipping of the coating was observed during the erosion test. Poor erosion resistance of the coating was probably due to presence of a network of cracks in the coating.

EXAMPLES FOR TUNGSTEN FOLLOWED BY TUNGSTEN/TUNGSTEN CARBIDE (W+W.sub.3 C) COATING

EXAMPLE 4A

In this example, a two step coating process was used. Several AM-350, Ti/6Al/4V and IN-718 specimens were heated to a temperature of about 460.degree. C. in the presence of flowing argon and at the reaction temperature a gaseous mixture of 300 cc/min WF.sub.6, and 3,000 cc/min of hydrogen was passed into the furnace over the specimens for 5 minutes to coat them with tungsten. After coating specimens with tungsten for 5 minutes, a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min hydrogen and 40 cc/min of DME was passed into the furnace for 55 minutes to provide tungsten/tungsten carbide coating. A total pressure was maintained at 40 Torr during tungsten as well as tungsten/tungsten carbide coating steps (see Table 2).

The stainless steel and Ti/6Al/4V specimens were coated with 2-3 .mu.m thick tungsten followed by 27-28 .mu.m thick tungsten/tungsten carbide coating as shown in Table 2. The tungsten/tungsten carbide top coat consisted of a mixture of W and W.sub.3 C phases as shown in Table 3. The hardness values of the coating on AM-350 and Ti/6Al/4V are summarized in Table 3. The coating on AM-350 and Ti/6Al/4V showed the presence of a network of cracks. Erosion resistance of the coating was extremely poor, as shown in Table 3. Additionally, extensive chipping of the coating was observed during the erosion test. Poor erosion resistance of the coating was probably due to extensive cracking of the coating.

This example described that providing a very thin interlayer of tungsten did not help in improving erosion resistance of the overall composite coating.

EXAMPLE 4B

The CVD run described in Example 4A was repeated to provide tungsten followed by tungsten/tungsten carbide coatings. The reaction conditions used in tungsten and tungsten/tungsten carbide coating steps are summarized in Table 2.

The stainless steel specimens were coated with 3 .mu.m tungsten followed by 25 .mu.m of tungsten/tungsten carbide. The top coat consisted of a mixture of W and W.sub.3 C phases. The coating showed the presence of a network of cracks. Erosion resistance of the coating improved slightly, but it was still extremely poor as shown in Table 3. Additionally, extensive chipping of the coating was observed during the erosion test. Poor erosion resistance was due to the presence of a network of cracks in the coating.

This example described that increasing the ratio of the thickness of the tungsten to the tungsten/tungsten carbide layer helped in improving the erosion resistance of the composite coating.

TABLE 3 __________________________________________________________________________ Example 2 Example 3 Example 4A Example 4B Example __________________________________________________________________________ 4C Experiment No. 50 36 37 33 42 Substrate AM-350 AM-350 AM-350 Ti/6A1/4V AM-350 AM-350 Ti/6A1/4V Coating Composition W W + W.sub.3 C W + W.sub.3 C W + W.sub.3 C W + W.sub.3 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer 455 .+-. 50 -- -- -- -- -- Tungsten/Tungsten Carbide -- 1788 .+-. 130 2276 .+-. 103 2150 .+-. 128 2333 .+-. 165 -- -- Layer Erosion Resistance Breakthrough Time, Secs 3 36 42 34 68 43 45 Calculated Erosion Rate, 6 42 40 31 69 84 82 secs/mil Weight Loss in 30 seconds, g -- 0.00036 -- -- 0.00040 -- -- __________________________________________________________________________ Example 4D Example 4E Example 4F Example 4G Example __________________________________________________________________________ 4H Experiment No. 38 107 104 106 164 Substrate AM-350 AM-350 AM-350 Ti/6A1/4V AM-350 AM-350 Ti/6A1/4V IN-718 Coating Composition W + W.sub.3 C W + W.sub.3 C W + W.sub.3 C W + W.sub.3 C W + W.sub.3 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- -- -- Tungsten/Tungsten Carbide 2164 .+-. 264 2395 .+-. 15 2361 .+-. 103 2328 .+-. 203 2470 .+-. 53 2424 2175 2539 Layer Erosion Resistance Breakthrough Time, Secs 89 93 115 93 95 128 115 109 Calculated Erosion Rate, 141 188 255 215 232 224 220 237 secs/mil Weight Loss in 30 seconds, g 0.00014 -- -- -- -- 0.00012 -- -- __________________________________________________________________________ Example 4I Example 4J Example __________________________________________________________________________ 4K Experiment No. 177 167 169 Substrate AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V IN-718 Coating Composition W + W.sub.3 C W + W.sub.3 C W + W.sub.3 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- -- -- -- Tungsten/Tungsten Carbide Layer 1930 1997 1971 2508 2516 2567 -- -- -- Erosion Resistance Breakthrough Time, Secs 69 70 70 94 93 96 45 34 42 Calculated Erosion Rate, secs/mil 227 228 231 274 262 271 260 252 266 Weight Loss in 30 seconds, g -- -- -- -- -- -- 0.00014 -- -- __________________________________________________________________________

EXAMPLE 4C

The CVD run described in Example 4A was repeated to provide tungsten followed by slightly thinner tungsten/tungsten carbide coatings. The reaction conditions used in tungsten and tungsten/tungsten carbide coating steps are summarized in Table 2.

The thicknesses of the tungsten and the tungsten/tungsten carbide layers obtained on AM-350 and Ti/6Al/4V are summarized in Table 2. The top coat of the coating consisted of a mixture of W and W.sub.3 C phases. The coating, once again, showed the presence of a network of cracks. However, the crack density was considerably lower than that observed in Examples 3, 4A and 4B. This suggested that the tungsten interlayer was helpful in reducing the crack density. The erosion resistance of the coating was considerably better then that of the coatings obtained in Examples 3, 4A and 4B (see Table 3). The extent of chipping observed during the erosion test also reduced considerably.

This example showed that increasing the ratio of the thickness of the tungsten layer to that of the tungsten/tungsten carbide layer from .about.0.07 to 0.12 in Examples 4A and 4B to .about.0.2 to 0.3 in this example unexpectedly reduced cracks in the coating and improved its erosion resistance.

EXAMPLE 4D

The CVD run described in Example 4A was once again repeated to provide tungsten followed by tungsten/tungsten carbide coating. The reaction conditions used for depositing tungsten and tungsten/tungsten carbide coatings were selected in such a way to provide a ratio of the thickness of the tungsten to the tungsten/tungsten carbide layers of .about.0.5 (see Table 2).

The coating showed the presence of cracks, but the crack density was greatly reduced. The coating, surprisingly, showed superior erosion resistance compared to Examples 3 and 4A to 4C. Furthermore, the composite coating obtained in this example showed significantly lower weight loss in the erosion resistance test than Example 3. The chipping of the coating observed during the erosion test was reduced dramatically as well. This example, therefore, clearly demonstrated the importance of the tungsten interlayer in reducing cracks and improving erosion resistance of the composite coating.

EXAMPLE 4E

In this example, reaction conditions for coating tungsten followed by tungsten/tungsten carbide were selected in such a way to provide a ratio of the thickness of the tungsten to the tungsten/tungsten carbide layers of .about.0.68 (see Table 2).

The composite coating showed the presence of only a few fine cracks (see FIG. 6). Etched cross section of the coating clearly showed columnar tungsten interlayer followed by non-columnar W+W.sub.3 C coating. The composite coating demonstrated superior erosion performance as shown in Table 3.

This example clearly demonstrated the importance of the tungsten interlayer in reducing cracks and improving erosion resistance of the composite coating.

EXAMPLE 4F

In this example, reaction conditions for coating tungsten followed by tungsten/tungsten carbide were selected in such a way to slightly increase the thickness ratio (see Table 2).

Once again, the coating on AM-350 and Ti/6Al/4V showed presence of a few cracks. Erosion resistance of the composite coating summarized in Table 3 was better than Example 4E. This example also demonstrated the importance of the tungsten interlayer in reducing cracks and improving erosion resistance.

EXAMPLE 4G

The CVD run described in Example 4F was repeated using reaction conditions summarized in Table 2 to provide slightly higher tungsten to tungsten/tungsten carbide coating thickness ratio.

Once again, the coating showed presence of a few fine cracks. Etched cross section of the coating clearly showed the presence of columnar tungsten interlayer and non-columnar tungsten/tungsten carbide top coat. The erosion resistance of the coating was very similar to that observed in Example 4F.

EXAMPLE 4H

The CVD run described in Example 4G was repeated using reaction conditions summarized in Table 2 to provide even higher tungsten to tungsten/tungsten carbide coating thickness ratio.

The coating on AM-350, Ti/6Al/4V and IN-718 showed presence of a few cracks. The erosion resistance of the coating was very similar to that noted in Examples 4F and 4G. The weight loss during the erosion test was considerably lower than that observed earlier.

This example, therefore, showed the importance of the tungsten interlayer in reducing the cracks in the coating and in improving the erosion resistance of the coating. It also showed that increasing the thickness of the tungsten interlayer to .about.16 .mu.m without increasing that of the tungsten/tungsten carbide did not help in further increasing the erosion resistance of the coating.

EXAMPLE 4I

The CVD run described in Example 4H was repeated to provide even higher tungsten to tungsten/tungsten carbide coating thickness ratio. The higher ratio was obtained by reducing the thickness of the tungsten/tungsten carbide layer.

The coating showed the presence of a few very fine cracks. The erosion resistance of the composite coating was similar to that noted in Example 4H (see Table 3). This example, once again, showed the importance of the tungsten interlayer in reducing cracks and improving erosion resistance of the composite coating. It also showed that the breakthrough time was dependent on the thickness of the tungsten/tungsten carbide layer; whereas, the erosion rate was independent of it.

EXAMPLE 4J

The CVD run described in Example 4I was repeated to provide even higher tungsten to tungsten/tungsten carbide coating thickness ratio. The higher ratio was obtained by increasing the thickness of the tungsten interlayer.

The coating, once again, showed presence of a few very fine cracks. The erosion resistance of the composite coating was slightly higher than that noted earlier (see Table 3). This example also showed the importance of the tungsten interlayer.

EXAMPLE 4K

The CVD run described in Example 4J was repeated to provide even higher tungsten to tungsten/tungsten carbide coating thickness ratio.

The coating, unexpectedly, was found to be absolutely crack free, as shown in the FIG. 7. The erosion resistance of the coating was comparable to the data noted earlier. Weight loss during erosion test was also comparable to the data noted earlier.

This example demonstrated that a crack-free coating could be obtained by manipulating the ratio of the thickness of the tungsten and the tungsten/tungsten carbide layers. This is an unexpected and significant finding.

Discussion on Tungsten Followed by W+W.sub.3 C Coating

Because of extensive cracking, the W+W.sub.3 C coating without a W interlayer provided very little erosion protection to the base metal. In this case, erosion occurs preferentially at cracks which causes chipping and flaking of large pieces of the coating. The cracks are believed to occur during the deposition and/or cool-down due to the build up in stresses within the coating. Surprisingly, the cracks in the coating can be minimized or even eliminated by providing a tungsten interlayer. It is believed that the function of the tungsten interlayer is to accommodate stresses that build up in the coating during the deposition and/or cool-down. The ability to accommodate stress may be in part due to the columnar structure of the tungsten layer, since the compliance of this layer is probably very anisotropic. The amount of coating stress which can be accommodated by the tungsten interlayer will depend on its thickness. However, the physical dimensions over which a significant amount of stress accommodation will occur will be limited so that the stresses which are present in the outer layer of a thick tungsten/tungsten carbide coating will be virtually unaffected by the presence of the interlayer. Consequently, both the thickness of the tungsten/tungsten carbide layer and the ratio of the W to the W+W.sub.3 C thickness are important in obtaining a crack-free composite coating.

The presence of a tungsten interlayer, in which the thickness of the tungsten interlayer is at least 3 .mu.m and the ratio of W to W+W.sub.3 C thickness is at least above 0.3, is necessary to increase the erosion resistance of the composite coating. However, the presence of a tungsten interlayer, in which the ratio of W to W+W.sub.3 C thickness is at least 0.6, is necessary for the optimum erosion and abrasion wear performance.

The tungsten interlayer also effects the performance of the tungsten/tungsten carbide coating in a scratch test. In this test, a diamond stylus is dragged across the surface of the sample at a constantly increasing load. The load at which coating loss begins to occur and the extent of coating loss can generally be correlated to the performance of a coating in the erosive and abrasive wear applications. The tungsten/tungsten carbide coating with no tungsten interlayer as described in Example 3 showed extensive coating loss in the 30-40 Newton load range in the scratch test, as shown in the FIG. 8. When a tungsten interlayer is present as described in Example 4E, the loss of the coating in the same load range is significantly reduced, as demonstrated in the FIG. 9; consequently, the presence of a tungsten interlayer is important for erosive and abrasive wear applications.

Due to the preferential erosive and abrasive wear, which occurs at cracks, a crack-free coating may be highly desirable under certain wear conditions. This conclusion would be especially true in situations where the substrate needs to be completely protected, such as in corrosive-wear environments. A crack-free coating will also be important when a smooth wear surface is required. This crack-free coating was unexpectedly obtained by significantly increasing the ratio of the thickness of the W to the W+W.sub.3 C layer. Although Example 4K was produced by depositing a thin layer of W+W.sub.3 C, in theory, a crack-free coating could also be produced by depositing a very thick tungsten interlayer.

EXAMPLES FOR TUNGSTEN/TUNGSTEN CARBIDE (W+W.sub.2 C+W.sub.3 C) COATING

EXAMPLE 5A

In this example, several AM-350 specimens were coated in a run. The specimens were heated to a temperature of about 460.degree. C. in the presence of flowing argon gas and at the reaction temperature a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min of hydrogen and 55 cc/min of DME was passed into the furnace over the specimens. The total pressure was maintained at 40 Torr, as shown in Table 4. The deposition was conducted for 20 minutes.

All the specimens were coated with a bright, smooth, adherent, coherent and uniform coating. The coating thickness was .about.7 .mu.m (see Table 4). It consisted of a mixture of W, W.sub.2 C and W.sub.3 C phases, which was considerably different than observed in Example 3. It was free of columnar grains. The micro-structure of the coating consisted of a layered structure. The coating had a smooth surface finish. However, the surface of the coating was cracked, as shown in the FIG. 10. The crack density was surprisingly lower than that observed in Example 3. The coating had a hardness of 2248 Vickers (Table 5). The coating showed poor erosion resistance; the breakthrough time and erosion rate were 21 seconds and 76 seconds/mil. The erosion resistance, however, was much higher than Example 3. The weight loss during erosion test was 0.00042 g in 30 seconds, which was very similar to that noted in Example 3. Extensive chipping of the coating was observed during the erosion test. Poor erosion resistance of the coating was probably due to the presence of a network of cracks in the coating.

EXAMPLE 5B

The CVD run described in Example 5A was repeated with Ti/6Al/4V specimens using reaction conditions described in Table 4. The specimens were coated with a bright, smooth, adherent, coherent and uniform .about.9.5 .mu.m thick coating. It consisted of a mixture of W, W.sub.2 C and W.sub.3 C phases. It was free of columnar grains. It had a smooth surface finish. It consisted of a network of cracks on the surface. It showed poor erosion resistance (see Table 5), but the erosion resistance was

TABLE 4 __________________________________________________________________________ Example 5A Example 5B Example 6A Example 6B Example __________________________________________________________________________ 6C Experiment No. 51 140 70 72 77 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Temperature, .degree.C. 460 460 460 465 465 Pressure, Torr 40 40 40 40 40 W Coating Conditions H.sub.2, SCCM -- -- 3,000 3,000 3,000 Ar, SCCM -- -- 4,500 4,500 4,500 WF.sub.6, SCCM -- -- 300 300 300 Time, Min. -- -- 3 4.5 10 Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 3,250 Ar, SCCM -- 1,800 -- -- -- WF.sub.6, SCCM 300 300 300 300 300 DME, SCCM 55 55 55 55 60 Time, Min. 20 35 20 20 45 Coating Thickness, .mu.m Tungsten -- -- 3.0 3.4 5.0 5.0 8.0 8.0 Tungsten/Tungsten Carbide 7.0 9.5 8.4 9.0 13.0 9.5 20.0 15.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide -- -- 0.36 0.38 0.38 0.52 0.40 0.53 Thickness Surface Topography Smooth, Many Smooth, Many Smooth, A Few Inter- Smooth, A Few Fine Smooth, A Interconnected Interconnected connected Cracks Cracks Few Cracks Cracks Cracks __________________________________________________________________________ Example 6D Example 6E Example 6F Example __________________________________________________________________________ 6G Experiment No. 53 103 82 111 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Temperature, .degree.C. 460 460 460 465 Pressure, Torr 40 40 40 40 W Coating Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 Ar, SCCM 4,000 4,500 4,500 4,500 WF.sub.6, SCCM 300 300 300 300 Time, Min. 7 15 10 15 Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,500 3,000 Ar, SCCM -- 300 -- 300 WF.sub.6, SCCM 300 300 350 300 DME, SCCM 55 60 65 50 Time, Min. 20 40 30 30 Coating Thickness, .mu.m Tungsten 6.0 6.0 9.2 7.7 9.0 8.6 9.6 8.8 Tungsten/Tungsten Carbide 9.5 9.5 12.3 12.3 16.0 11.5 11.5 12.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide 0.63 0.63 0.74 0.63 0.56 0.75 0.83 0.73 Thickness Surface Topography Smooth, Smooth, Smooth, A Few Fine Smooth, A Few Fine Smooth, A Few Fine No A Few Cracks Cracks Cracks Cracks Cracks __________________________________________________________________________ Example 6H Example 6I Example 6J Example __________________________________________________________________________ 6K Experiment No. 102 52 56 76 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Temperature, .degree.C. 460 460 460 465 Pressure, Torr 40 40 40 40 W Coating Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 Ar, SCCM 4,500 4,000 4,500 4,000 WF.sub.6, SCCM 300 300 300 300 Time, Min. 15 10 10 30 Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 Ar, SCCM 300 -- -- -- WF.sub.6, SCCM 300 300 300 300 DME, SCCM 60 55 55 55 Time, Min. 30 20 15 45 Coating Thickness, .mu.m Tungsten 10.0 8.1 8.0 7.5 7.1 7.5 19.0 16.0 Tungsten/Tungsten Carbide 8.0 8.0 10.0 7.5 6.2 6.0 11.0 9.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide 1.25 1.01 0.80 1.00 1.14 1.25 1.75 1.78 Thickness Surface Topography Smooth, No Cracks Smooth, No Cracks Smooth, No Cracks Smooth, No __________________________________________________________________________ Cracks

TABLE 5 __________________________________________________________________________ Example 5A Example 5B Example 6A Example __________________________________________________________________________ 6B Experiment No. 51 140 70 72 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Coating Composition W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- Tungsten/Tungsten Carbide Layer 2248 .+-. 70 2191 2078 .+-. 49 -- 2253 ---. 73 Erosion Resistance Breakthrough Time, secs 21 44 104 131 160 147 Calculated Erosion Rate, 76 117 314 370 313 394 secs/mil Weight Loss in 0.00042 0.0028 0.00012 0.00015 -- -- 30 seconds, g __________________________________________________________________________ Example 6C Example 6D Example __________________________________________________________________________ 6E Experiment No. 77 53 103 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Coating Composition W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- Tungsten/Tungsten Carbide Layer 2102 .+-. 101 -- 2359 .+-. 114 2215 .+-. 194 2224 2469 .+-. 53 Erosion Resistance Breakthrough Time, secs 218 201 119 -- 158 137 Calculated Erosion Rate, 278 340 318 -- 325 283 secs/mil Weight Loss in -- -- -- -- -- -- 30 seconds, g __________________________________________________________________________ Example 6F Example 6G Example __________________________________________________________________________ 6H Experiment No. 82 111 102 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Coating Composition W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- Tungsten/Tungsten Carbide Layer 2220 .+-. 100 -- 3097 .+-. 210 3156 .+-. 76 2167 2324 .+-. 50 Erosion Resistance Breakthrough Time, secs 209 128 146 123 67 66 Calculated Erosion Rate, 332 284 322 260 212 208 secs/mil Weight Loss in -- -- -- -- -- -- 30 seconds, g __________________________________________________________________________ Example 6I Example 6J Example __________________________________________________________________________ 6K Experiment No. 52 56 76 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Coating Composition W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C W + W.sub.2 C + W.sub.3 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- Tungsten/Tungsten Carbide Layer 2091 .+-. 101 2155 .+-. 20 2078 .+-. 66 -- -- 2091 .+-. 98 Erosion Resistance Breakthrough Time, secs 125 73 58 91 158 150 Calculated Erosion Rate, 317 248 237 383 364 423 secs/mil Weight Loss in 0.00012 0.00014 -- -- -- -- 30 seconds, g __________________________________________________________________________

TABLE 6 __________________________________________________________________________ Example 7A Example 7B Example 7C __________________________________________________________________________ Experiment No. 69 121 115 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V IN-718 Temperature, .degree.C. 460 440 460 Pressure, Torr 40 40 40 W Coating Conditions H.sub.2, SCCM 3,000 2,500 3,000 Ar, SCCM 4,500 5,500 4,500 WF.sub.6, SCCM 300 250 300 Time, Min. 15 15 10 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 Ar, SCCM -- 1,800 300 WF.sub.6, SCCM 300 300 300 DME, SCCM 85 90 90 Time, Min. 70 115 40 Coating Thickness, .mu.m Tungsten 8.0 10.0 6.8 6.0 6.3 4.8 4.6 5.0 Tungsten/Tungsten Carbide 23.0 23.0 17.0 16.0 15.0 11.0 10.0 10.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide 0.35 0.43 0.40 0.37 0.42 0.44 0.46 0.50 Thickness Surface Topography Smooth, A few fine Smooth, a few Fine Smooth, Smooth, Smooth, Interconnected Cracks No Cracks Fine Noacks Cracks Cracks __________________________________________________________________________ Example 7D Example 7E Example 7F Example __________________________________________________________________________ 7G Experiment No. 95 120 119 91 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Temperature, .degree.C. 460 445 450 460 Pressure, Torr 40 40 40 40 W Coating Conditions H.sub.2, SCCM 3,000 2,500 2,500 3,000 Ar, SCCM 4,500 5,500 5,500 4,500 WF.sub.6, SCCM 300 250 250 300 Time, Min. 10 15 15 10 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 Ar, SCCM 300 1,800 1,500 300 WF.sub.6, SCCM 300 300 300 300 DME, SCCM 90 90 90 90 Time, Min. 50 95 80 40 Coating Thickness, .mu.m Tungsten 6.6 4.4 6.8 6.2 6.4 6.8 6.8 5.6 5.0 Tungsten/Tungsten Carbide 14.8 12.0 13.0 12.7 10.6 12.4 12.8 10.0 10.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide 0.44 0.37 0.52 0.49 0.60 0.55 0.53 0.56 0.50 Thickness Surface Topography Smooth, Fine Cracks Smooth, No Cracks Smooth, No Cracks Smooth, No __________________________________________________________________________ Cracks Example 7H Example 7I Example __________________________________________________________________________ 7J Experiment No. 97 122 68 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V Temperature, .degree.C. 460 460 460 Pressure, Torr 40 40 40 W Coating Conditions H.sub.2, SCCM 3,000 2,500 3,000 Ar, SCCM 4,500 5,500 4,500 WF.sub.6 , SCCM 300 250 300 Time, Min. 15 25 30 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 Ar, SCCM 300 1,500 -- WF.sub.6, SCCM 300 300 300 DME, SCCM 90 90 85 Time, Min. 50 85 70 Coating Thickness, .mu.m Tungsten 9.0 7.0 12.4 12.3 12.1 25.0 23.0 Tungsten/Tungsten Carbide 15.0 11.5 19.1 18.3 17.5 27.0 26.0 Tungsten Coating Thickness Tungsten/Tungsten Carbide 0.60 0.61 0.65 0.67 0.69 0.93 0.88 Thickness Surface Topography Smooth, Smooth, Smooth, Cracks Smooth, Cracks Cracks No Cracks __________________________________________________________________________ Example 7K Example 7L Example 7M Example __________________________________________________________________________ 7N Experiment No. 123 100 101 63 Substrate AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Temperature, .degree.C. 460 460 460 460 Pressure, Torr 40 40 40 40 W Coating Conditions H.sub.2, SCCM 2,500 3,000 3,000 3,000 Ar, SCCM 5,500 4,500 4,500 4,500 WF.sub.6, SCCM 250 300 300 300 Time, Min. 18 15 15 10 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 3,000 3,000 Ar, SCCM 1,800 300 300 300 WF.sub.6, SCCM 300 300 300 300 DME, SCCM 90 80 70 85 Time, Min. 65 40 40 20 Coating Thickness, .mu.m Tungsten 8.8 9.0 9.2 12.0 10.4 11.2 9.2 7.5 6.7 Tungsten/Tungsten Carbide 12.7 13.1 12.3 11.6 10.4 10.0 9.2 7.7 6.5 Tungsten Coating Thickness Tungsten/Tungsten Carbide 0.69 0.68 0.75 1.03 1.00 1.12 1.00 0.97 1.03 Thickness Surface Topography Smooth, No Cracks Smooth, No Cracks Smooth, No Cracks Smooth, No __________________________________________________________________________ Cracks Example 7O Example __________________________________________________________________________ 7P Experiment No. 65 90 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Temperature, .degree.C. 460 460 Pressure, Torr 40 40 W Coating Conditions H.sub.2, SCCM 3,000 3,000 Ar, SCCM 4,500 4,500 WF.sub.6, SCCM 300 300 Time, Min. 5 10 Tungsten/Tungsten Carbide Conditions H.sub.2, SCCM 3,000 3,000 Ar, SCCM 300 300 WF.sub.6, SCCM 300 300 DME, SCCM 90 90 Time, Min. 20 30 Coating Thickness, .mu.m Tungsten 4.0 4.0 5.6 5.2 Tungsten/Tungsten Carbide 6.2 5.9 7.6 7.4 Tungsten Coating Thickness Tungsten/Tungsten Carbide 0.64 0.68 0.74 0.70 Thickness Surface Topography Smooth, No Cracks Smooth, No __________________________________________________________________________ Cracks

TABLE 7 __________________________________________________________________________ Example 7A Example 7B Example 7C __________________________________________________________________________ Experiment No. 69 121 115 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V IN-718 Coating Composition W + W.sub.2 C W + W.sub.2 C W + W.sub.2 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- -- -- Tungsten/Tungsten 3060 .+-. 230 2792 .+-. 60 2470 .+-. 53 2432 .+-.53 2588 .+-. 57 2850 .+-. 66 2947 ---. 71 Carbide Layer Erosion Resistance Breakthrough Time, secs -- 304 201 214 183 135 126 116 Calculated Erosion Rate, -- 336 300 339 310 312 319 295 secs/mil Weight Loss in -- -- 0.00018 0.00020 0.00024 -- -- -- 30 seconds, g __________________________________________________________________________ Example 7D Example 7E Example __________________________________________________________________________ 7F Experiment No. 95 120 119 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V Coating Composition W + W.sub.2 C W + W.sub.2 C W + W.sub.2 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- -- Tungsten/Tungsten 2991 .+-. 63 3106 .+-. 148 2628 .+-. 15 2507 .+-. 20 2402 .+-. 160 2469 .+-. 53 2395 .+-. 15 Carbide Layer Erosion Resistance Breakthrough Time, secs 203 149 132 135 112 165 154 Calculated Erosion Rate, 349 311 258 270 284 325 306 secs/mil Weight Loss in -- -- -- -- -- -- -- 30 seconds, g __________________________________________________________________________ Example 7G Example 7H Example 7I __________________________________________________________________________ Experiment No. 91 97 122 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V IN-718 Coating Composition W + W.sub.2 C W + W.sub.2 C W + W.sub.2 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- -- Tungsten/Tungsten 3089 .+-. 89 2767 .+-. 188 2908 .+-. 213 2758 .+-. 15 2472 .+-. 110 2507 .+-. 15 2432 .+-. 53 Carbide Layer Erosion Resistance Breakthrough Time, secs 124 113 182 150 259 234 248 Calculated Erosion Rate, 315 288 308 331 345 325 361 secs/mil Weight Loss in -- -- -- -- -- -- -- 30 seconds, g __________________________________________________________________________ Example 7J Example 7K Example __________________________________________________________________________ 7L Experiment No. 68 123 100 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V IN-718 AM-350 Ti/6A1/4V Coating Composition W + W.sub.2 C W + W.sub.2 C W + W.sub.2 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- Tungsten/Tungsten 2758 .+-. 31 2689 .+-. 159 2398 .+-. 109 2324 .+-. 50 2511 .+-. 116 2758 .+-. 15 2758 .+-. 15 Carbide Layer Erosion Resistance Breakthrough Time, secs 356 325 162 172 143 144 120 Calculated Erosion Rate, 335 318 325 328 295 316 293 secs/mil Weight Loss in -- -- 0.00016 0.00018 0.00014 -- -- 30 seconds, g __________________________________________________________________________ Example 7M Example 7N Example 7O Example __________________________________________________________________________ 7P Experiment No. 101 62 65 90 Substrate AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V AM-350 Ti/6A1/4V Coating Composition W + W.sub.2 C W + W.sub.2 C W + W.sub.2 C W + W.sub.2 C Coating Hardness, Kg/mm.sup.2 Tungsten Layer -- -- -- -- -- -- -- -- Tungsten/Tungsten 2434 .+-. 102 2510 .+-. 95 2746 .+-. 51 -- 2758 .+-. 50 -- 2660 2716 .+-. 163 Carbide Layer Erosion Resistance Breakthrough Time, secs 125 125 -- 65 54 65 92 73 Calculated Erosion Rate, 317 345 -- 254 221 280 307 250 secs/mil Weight Loss in -- -- -- -- -- -- -- -- 30 seconds, g __________________________________________________________________________

This example showed that the erosion resistance of W+W.sub.2 C coating with a W interlayer was much better than that of W+W.sub.3 C and W+W.sub.2 C+W.sub.3 C coatings with a W interlayer. This is an unexpected and significant finding.

EXAMPLE 7B

In this example, several AM-350, Ti/6Al/4V and IN-718 specimens were coated with W followed by W+W.sub.2 C coating using conditions summarized in Table 6. All the specimens were coated with .about.6 .mu.m and .about.15 .mu.m W and W+W.sub.2 C layers, respectively. The coating consisted of columnar W coating and non-columnar W+W.sub.2 C coating at the top of W. The thickness ratio was .about.0.4. The coating was smooth. However, a few fine cracks were noted in the coating, as shown in the FIG. 12. The erosion resistance of the coating shown in Table 7 was similar to that noted in Example 7A. The weight loss during erosion test was determined and presented in Table 7. The weight loss was slightly higher in this example than that observed with W+W.sub.2 C+W.sub.3 C coating with W interlayer. This could be related to the fact the cracks in W+W.sub.2 C coatings were slightly wider than those noted in W+W.sub.2 C+W.sub.3 C coating.

Examples 7A and 7B clearly showed that a tungsten to tungsten/tungsten carbide thickness ratio of .about.0.35 is sufficient enough to give a maximum erosion resistance.

EXAMPLE 7C

The CVD run described in Example 7B was repeated to provide slightly higher thickness ratio. The thickness of W+W.sub.2 C layer varied from 10 .mu.m to 11 .mu.m on various substrates, and the ratio varied from 0.44 to 0.50. The coating on AM-350 and IN-718 was crack-free; whereas, a few fine cracks were observed on Ti/6Al/4V. This indicated that crack-free coating on AM-350 and IN-718 can be obtained by providing .about.5 .mu.m thick W and .about.10 to 11 .mu.m thick W+W.sub.2 C layers. These thickness values, however, were not good enough to give crack-free coating on Ti/6Al/4V. The erosion resistence of the coating was very good as shown in Table 7.

EXAMPLE 7D

The CVD run described in Example 7C was repeated to provide slightly thicker W+W.sub.2 C layer while maintaining thickness ratio. Surprisingly, the coating on AM-350 and Ti/6Al/4V cracked. This information suggested that the thickness of W+W.sub.2 C layer was important to prevent cracks in the coating. The erosion resistance of the coating was good, as shown in Table 7.

EXAMPLE 7E

The CVD run described in Example 7D was repeated to provide slightly thinner W+W.sub.2 C layer and slightly higher thickness ratio. The coating on AM-350, Ti/6Al/4V and IN-718 was absolutely crack-free (see FIG. 13), certifying the importance of the thickness of W+W.sub.2 C. The unetched and etched cross-sectional views of the composite coatings are shown in the FIGS. 3 and 4. The etched cross-section presented in the FIG. 4 showed columnar growth of the tungsten interlayer and the non-columnar growth of the tungsten/tungsten carbide layer. The etched cross-section of the coating also demonstrated the absence of any cracks in the coating. The erosion resistance of the coating was good, as shown in Table 7.

EXAMPLES 7F AND 7G

The CVD run described in Example 7E was repeated in these examples to verify the concept of crack-free coating. The coatings obtained in these runs were absolutely crack-free. They also had good erosion resistance, as shown in Table 7.

EXAMPLE 7H

In this example, the thickness of W and W+W.sub.2 C layers was slightly increased on AM-350 stainless steel to determine its effect on cracks. The thickness ratio obtained was .about.0.6. The coating on AM-350 cracked and that on Ti/6Al/4V did not. The coating on AM-350 cracked probably because of the thicker W+W.sub.2 C layer. This information further confirmed the statement made earlier that the thickness of W+W.sub.2 C layer played an important role in obtaining crack-free coating. Erosion resistance of the coating was good, as shown in Table 7.

EXAMPLE 7I

To further demonstrate the effect of W+W.sub.2 C coating thickness on cracks, a CVD run was carried out to obtain a thicker W+W.sub.2 C coating and a higher thickness ratio. Despite higher thickness ratio the coating on all the specimens cracked. This example, therefore, confirmed the importance of the thickness of W+W.sub.2 C layer for preventing cracks in the coating. The erosion resistance of the coating was good, as expected.

EXAMPLE 7J

To further demonstrate the effect of W+W.sub.2 C coating thickness on cracks, one more CVD run was conducted to obtain thicker W+W.sub.2 C coating and higher thickness ratio. Once again, coating cracked. The erosion resistance of the coating, however, was still good.

EXAMPLES 7K TO 7P

Several CVD runs were conducted to vary thicknesses of W and W+W.sub.2 C layers and thickness ratios. These experiments were conducted to effectively map out the crack-free and cracked coating region. The data summarized in Table 6 showed that as long as the thickness of W+W.sub.2 C layer was maintained below .about.13.5 .mu.m and thickness ratio maintained above 0.6 the coating obtained was absolutely crack-free. The coating in all the cases demonstrated good erosion resistance, as shown in Table 7.

Discussion on Tungsten Followed by W+W.sub.2 C Coating

The erosion resistance of the W+W.sub.2 C coating is either equivalent to or superior to the erosion resistance of W+W.sub.2 C+W.sub.3 C. The erosion resistance of W+W.sub.2 C is independent of the thickness of the tungsten interlayer when the ratio of the W to the W+W.sub.2 C thickness is at least 0.35.

Careful control of both the thickness of the tungsten/tungsten carbide coating and the ratio of the thicknesses of W to W+W.sub.2 C is required to obtain a crack-free coating. For both AM-350 and Ti/6Al/4V, the maximum thickness for producing a crack-free coating is about 14 .mu.m. The critical thickness ratio for a crack-free coating is about 0.4 and 0.5 for AM-350 and Ti/6Al/4V, respectively.

EXAMPLE 8

The wear performance of the uncoated stainless steel 1" diameter SS-422 disc was determined using a ball-on-disc test in the presence and absence of a lubricant. The non-lubricated wear test was conducted in dry air (1% relative humidity) and saturated air (99% relative humidity). The lubricated wear test was conducted in the presence of a cutting fluid consisting of an emulsion of 20% mineral oil in water. The ball used in the test was made of 52-100 chrome steel. The ball-on-disc wear test was performed using a load of 5 Newton, ambient temperature, stationary ball on rotating disc at a speed of 10 cm/sec., and for approximately 0.3 kilometer. The wear performance was determined by measuring the combined volumetric material loss of the ball and disc. The wear rate was very high in the dry air (1% relative humidity), as shown in the Table 8. The wear rate in the saturated air (99% relative humidity) and cutting fluid, on the other hand, was considerably lower, with the rate being lowest in the presence of the lubricant.

EXAMPLE 9

In this example, a two-step coating process was used. Several SS-422 discs were heated to a temperature of bout 460.degree. C. in the presence of flowing argon and at the reaction temperature a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min hydrogen, and 4,500 cc/min of argon was passed into the furnace over the specimens for 15 minutes to coat them with tungsten. After coating the specimens with tungsten for 15 minutes, a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min hydrogen, 300 cc/min argon and 40 cc/min of DME was passed into the furnace for 30 minutes to provide tungsten/tungsten carbide coating. A total pressure was maintained at 40 Torr during the tungsten as well as tungsten/tungsten carbide coating steps.

The SS-422 discs were coated with 10.4 .mu.m thick tungsten followed by 12.4 .mu.m thick tungsten/tungsten carbide. The tungsten/tungsten carbide top coat consisted of a mixture of W and W.sub.3 C phases. The hardness of the top coat was approximately 2450 Vickers. The coating was smooth and had a few very fine interconnected cracks.

The wear performance of the coated SS-422 disc was determined using ball-on-disc test described in the Example 8 in the presence of 1% and 99% relative humidity and cutting fluid as a lubricant. The wear rate data summarized in the Table 8 showed dramatically lower wear rate in the presence of dry air (1% relative humidity) compared to the uncoated disc. The wear rate in the presence of 99% relative humidity and cutting fluid was also lower than the uncoated disc.

This example, therefore, shows that a composite coating is very effective in reducing the total wear rate in the presence and absence of a lubricant.

EXAMPLE 10

In this example, a two-step coating process was used again. Several SS-422 discs were heated to a temperature of about 460.degree. C. in the presence of flowing argon and at the reaction temperature a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min hydrogen, and 4,500 cc/min of argon was passed into the furnace over the specimens for 15 minutes to coat them with tungsten. After coating the specimens with tungsten for 15 minutes, a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min hydrogen, 300 cc/min argon and 60 cc/min of DME was passed into the furnace for 40 minutes to provide tungsten/tungsten carbide coating. A total pressure was maintained at 40 Torr during the tungsten as well as tungsten/tungsten carbide coating steps.

The SS-422 discs were coated with 9.7 .mu.m thick tungsten followed by 14.0 .mu.m thick tungsten/tungsten carbide. The tungsten/tungsten carbide top coat consisted of a mixture of W, W.sub.2 C and W.sub.3 C phases. It had a hardness of approximately 2250 Vickers. The coating was smooth and had a few extremely fine and long cracks.

TABLE 8 __________________________________________________________________________ Composition of the Tungsten/Tungsten Total Wear Rate, 10.sup.-15 m.sup.2 /N Example No. Carbide Top Coat 1% Humidity 99% Humidity Cutting Fluid __________________________________________________________________________ Example 8 -- 327 8.1 2.9 Example 9 W + W.sub.3 C 1.9 7.7 1.0 Example 10 W + W.sub.2 C + W.sub.3 C 1.0 4.7 0.9 Example 11 W + W.sub.2 C 1.40 3.6 1.0 __________________________________________________________________________

The wear performance of the coated SS-422 disc was determined using ball-on-disc test described in the Example 8 in the presence of 1% and 99% relative humidity and cutting fluid as a lubricant. The wear rate data summarized in the Table 8 showed lower wear rate in the presence of 1% and 99% relative humidity and cutting fluid compared to the uncoated disc and disc coated with tungsten followed by W+W.sub.3 C coating.

This example shows that a composite coating is very effective in improving wear performance of the SS-422 disc. It also shows that the wear performance of the composite coating can be improved by adjusting the composition of the tungsten/tungsten carbide top coat.

EXAMPLE 11

In this example, a two-step coating process was used again. Several SS-422 discs were heated to a temperature of about 460.degree. C. in the presence of flowing argon and at the reaction temperature a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min hydrogen, and 4,500 cc/min of argon was passed into the furnace over the specimens for 15 minutes to coat them with tungsten. After coating the specimens with tungsten for 15 minutes, a gaseous mixture of 300 cc/min WF.sub.6, 3,000 cc/min hydrogen, 300 cc/min argon and 80 cc/min of DME was passed into the furnace for 40 minutes to provide tungsten/tungsten carbide coating. A total pressure was maintained at 40 Torr during the tungsten as well as tungsten/tungsten carbide coating steps.

The SS-422 discs were coated with 10 .mu.m thick tungsten followed by 13.0 .mu.m thick tungsten/tungsten carbide. The tungsten/tungsten carbide top coat consisted of a mixture of W and W.sub.2 C phases. It had a hardness of approximately 2750 Vickers. The coating was smooth and crack-free.

The wear performance of the coated SS-422 disc was determined using ball-on-disc test described in Example 8 in the presence of 1% and 99% relative humidity and cutting fluid as a lubricant. The wear rate data summarized in Table 8 showed the wear rate was similar to that noted with the other composite coatings (i.e., W+W.sub.3 C and W+W.sub.2 C+W.sub.3 C coatings) in the presence of dry air (1% relative humidity) and cutting fluid. The wear rate, however, was lower compared to other composite coatings in the presence of 99% relative humidity.

This example shows that a composite coating is very effective in improving wear performance of the SS-422 disc.

General Discussion

The wear data presented in Examples 8 to 11 clearly demonstrate that a composite tungsten followed by tungsten/tungsten carbide coating can be used to significantly reduce the abrasive wear rate and concomitantly increase the life of the stainless steel material in the dry, humid and lubricated environments. The data presented in Examples 1 to 4 show that the composite coating is very effective in reducing the erosive wear rate of the ferrous and non-ferrous alloys. Additionally, Examples 1 to 4 show that an interlayer of tungsten is required to improve the performance of the tungsten/tungsten carbide coating. This is an unexpected finding.

The relationship between the ratio of the thickness of the tungsten interlayer to the thickness of the tungsten-carbon alloy (tungsten/tungsten carbide coating) is elaborated further in the FIG. 14. It shows that for W+W.sub.3 C top coat the erosion resistance measured as secs/mil increases with increasing the thickness ratio. A thickness ratio greater than 0.3 is required to significantly increase the erosion resistance of the W+W.sub.3 C coating system. Furthermore, a thickness ratio of about 0.6 is required to obtain optimum erosion resistance of the W+W.sub.3 C coating system. FIG. 14 also shows that a thickness ratio of greater than 0.3 is required for significantly increasing the erosion resistance of the W+W.sub.2 C+W.sub.3 C coating system. It also shows that a thickness ratio of about 0.35 yields optimum erosion performance both for the W+W.sub.2 C+W.sub.3 C and W+W.sub.2 C coating systems. This thickness ratio to obtain optimum erosion resistance is considerably lower for the W+W.sub.2 C+W.sub.3 C and W+W.sub.2 C coating systems than the W+W.sub.3 C coating system.

The relationship between the thickness of the tungsten-carbon alloy and the ratio of the thickness of the tungsten interlayer to the thickness of the tungsten-carbon alloy (tungsten/tungsten carbide coating) is presented in FIG. 15. It shows a very narrow region for obtaining a crack-free W+W.sub.3 C coating system. A thin W+W.sub.3 C layer is required to achieve a crack-free coating. Compared to the W+W.sub.3 C coating system, the W+W.sub.2 C+W.sub.3 C and W+W.sub.2 C coating systems provide a wider crack-free coating region.

It is worth noting that a thicker crack-free tungsten/tungsten carbide coating can be obtained for W+W.sub.2 C top coat than is possible for W+W.sub.2 C+W.sub.3 C or for W+W.sub.3 C. In addition, the thickness of the tungsten interlayer which is required to achieve a crack-free coating is significantly lower for W+W.sub.2 C than for W+W.sub.2 C+W.sub.3 C or W+W.sub.3 C. By reducing the thickness of the W interlayer, the overall thickness of the composite coating which is required to provide a specified erosive wear life or abrasive wear life can be minimized by going progressively from W+W.sub.3 C to W+W.sub.2 C+W.sub.3 C and to W+W.sub.2 C composite coating system.

One particularly important use of the composite coating system according to the present invention is to provide highly erosive and abrasive wear resistant coatings on ferrous, non-ferrous and titanium alloy compressor blades for gas turbines and jet engines.

Claims

What is claimed is:

1. A method for producing a highly erosion and abrasion wear resistant composite coating system on a substrate selected from the group consisting of ferrous metals and alloys, non-ferrous metals and alloys, graphite, carbides and ceramics, comprising, chemical vapor depositing on the substrate a substantially columnar, intermediate layer of tungsten of sufficient thickness to confer substantial wear resistant characteristics on said coating system using a gaseous mixture of tungsten halide and hydrogen at pressures within the range of about 1 Torr. to about 1,000 Torr and a temperature of about 300.degree. to about 650.degree. C., and chemical vapor depositing on said intermediate layer a non-columnar, substantially lamellar outer layer of a mixture of tungsten and tungsten carbide using a gaseous mixture of tungsten halide, hydrogen and an oxygen-containing hydrocarbon at pressures within the range of 1 Torr to about 1,000 Torr and temperatures within the range of about 300.degree. to about 650.degree. C., with said tungsten carbide comprising W.sub.2 C, W.sub.3 C or a mixture of both, wherein the ratio of the thickness of the tungsten intermediate layer to the thickness of the outer layer is at least 0.35 in the case of tungsten plus W.sub.2 C in the outer layer, 0.60 in the case of tungsten plus W.sub.3 C in the outer layer and, 0.35 in the case of mixtures of tungsten and W.sub.2 C and W.sub.3 C in the outer layer.

2. A method according to claim 1 wherein said intermediate layer is at least about two microns thick.

3. A method according to claim 1 wherein a primary layer comprised nickel is deposited on the substrate prior to deposition of the intermediate layer.

4. The highly erosion and abrasion wear resistant composite coating system on a substrate prepared in accordance with the method of claim 1 for use as compressor blades for gas turbines and jet engines.